Piper PA 28-181 Manual page 35

SECTION 1
NORMAL PROCEDURES
PIPER AIRCRAFT CORPORATION
PA.2t.I6I. ARCHER II
Performance for a specific airplane may vary from published figures
dep€nding upon the equipmeni insralled, rhe condition of the engine,
airplan€ and eqüipm€nt, atmospheric conditions and piloring technique.
B e s t R a t e o f C l i m b S p e € d . . . , . . , . . . . . . . . . . . . . . . . . . ? 6 K I A S
Best Angle of Climb Speed . . . . . . . . . . . . . . . . . . . . . . . . 64 KIAS
Turbulent Air Op€rating Speed (S€e
S u b s e c t i o n
2 . 3 ) , . , , . . . .
. . . . .
3 K I A S
Maximum Flap Speed
. . . .. 102 KIAS
Landins Final Approach Speed (naps a0.) . .. .. .. .. .66 KIAS
M a x i m u m D e m o n s t r a t e d
C r o s s w i n d V e l o c i t v . . , . , . . . . l 7
K T S
(b)
tc,
(d)
(0
Rf,PORT: vB-1120
4-2
ISSUED: JULY 2, 1979